標題: Titlebook: Aerodynamics of Tandem Wing Aircraft; From Dinosaurs to UA Illia S. Kryvokhatko Book 2025Latest edition The Editor(s) (if applicable) and T [打印本頁] 作者: hedonist 時間: 2025-3-21 19:22
書目名稱Aerodynamics of Tandem Wing Aircraft影響因子(影響力)
書目名稱Aerodynamics of Tandem Wing Aircraft影響因子(影響力)學科排名
書目名稱Aerodynamics of Tandem Wing Aircraft網(wǎng)絡(luò)公開度
書目名稱Aerodynamics of Tandem Wing Aircraft網(wǎng)絡(luò)公開度學科排名
書目名稱Aerodynamics of Tandem Wing Aircraft被引頻次
書目名稱Aerodynamics of Tandem Wing Aircraft被引頻次學科排名
書目名稱Aerodynamics of Tandem Wing Aircraft年度引用
書目名稱Aerodynamics of Tandem Wing Aircraft年度引用學科排名
書目名稱Aerodynamics of Tandem Wing Aircraft讀者反饋
書目名稱Aerodynamics of Tandem Wing Aircraft讀者反饋學科排名
作者: 和平主義 時間: 2025-3-21 23:37
Hervé Bredin,Aurélien Mayoue,Gérard Cholletical method is presented. Its main advantage over previous theoretical approaches is the possibility to evaluate roll moment, as well as moderate dihedral angles and sweep angles of the wings. Also, it takes into account the contraction of tip vortices to the symmetry plane that improves the accurac作者: Lament 時間: 2025-3-22 03:56
Text-independent Speaker Verification,larly, subchapters consider high-wing and low-wing, wingspan ratio, airfoils and angles of their setting, stagger and vertical gap between the wings, and wings’ dihedral angles. There is research on wingtip devices installed on forward and rear wings that affect not only lift-drag ratio but all thre作者: Musculoskeletal 時間: 2025-3-22 06:42
Creating and Maintaining Databasest is better to consider the conventional scheme, or canard, or flying wing). Then, how to choose the overall layout and dimensions of the tandem wing aircraft as the design process differs greatly from the one for a classical aircraft. Next, principal suggestions are listed if there is a need to (1)作者: 易達到 時間: 2025-3-22 10:19
https://doi.org/10.1007/978-3-031-74809-7Tandem Wing Aircraft; Aerodynamics; UAVs; four-winged aircraft; canard作者: 預(yù)感 時間: 2025-3-22 16:16
978-3-031-74811-0The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Switzerl作者: Daily-Value 時間: 2025-3-22 19:24 作者: FIG 時間: 2025-3-23 00:42
http://image.papertrans.cn/b/image/167338.jpg作者: 使腐爛 時間: 2025-3-23 05:25
rstanding of the history of aircraft development, including .This updated, second edition adds more reviews of modern four-winged aircraft belonging to convertiplanes, Medium Altitude Long Endurance UAVs, and solar planes. As in the first edition, different analytical, numerical, and experimental me作者: cogitate 時間: 2025-3-23 05:35
Book 2025Latest editionolar planes. As in the first edition, different analytical, numerical, and experimental methods are discussed in detail. ?The book presents new sections on unsteady aerodynamic characteristics of tandem wings and specifics of their aerodynamic loading for stress analysis and structural design. Also,作者: LVAD360 時間: 2025-3-23 12:12 作者: 相一致 時間: 2025-3-23 16:05 作者: PAEAN 時間: 2025-3-23 18:14 作者: indecipherable 時間: 2025-3-24 00:18
Creating and Maintaining Databasester of gravity range backward/forward, (4) expand a range of the center of gravity, (5) increase rolling stability, (6) increase directional (yawing) stability. The second edition of the book was updated on new studies that were reflected in the recommendations.作者: MOTTO 時間: 2025-3-24 05:20 作者: Heretical 時間: 2025-3-24 09:56
Effect of Geometric Parameters on Aerodynamic Characteristics, different sweep angles of the wings immediately after its release). The second edition is complemented by numerical research on aerodynamic loading where specifics for forward and rear wings due to their interference have been found.作者: 法律 時間: 2025-3-24 14:00
Recommendations Regarding Aerodynamic Design of Tandem Wing Aircraft,ter of gravity range backward/forward, (4) expand a range of the center of gravity, (5) increase rolling stability, (6) increase directional (yawing) stability. The second edition of the book was updated on new studies that were reflected in the recommendations.作者: 沉思的魚 時間: 2025-3-24 16:25 作者: antidepressant 時間: 2025-3-24 21:35
Determination of Tandem Wing Aircraft Aerodynamic Characteristics,ical method is presented. Its main advantage over previous theoretical approaches is the possibility to evaluate roll moment, as well as moderate dihedral angles and sweep angles of the wings. Also, it takes into account the contraction of tip vortices to the symmetry plane that improves the accurac作者: Obverse 時間: 2025-3-25 02:52 作者: 壁畫 時間: 2025-3-25 06:37
Recommendations Regarding Aerodynamic Design of Tandem Wing Aircraft,t is better to consider the conventional scheme, or canard, or flying wing). Then, how to choose the overall layout and dimensions of the tandem wing aircraft as the design process differs greatly from the one for a classical aircraft. Next, principal suggestions are listed if there is a need to (1)作者: jeopardize 時間: 2025-3-25 09:42
Determination of Tandem Wing Aircraft Aerodynamic Characteristics,cription of a wind tunnel model of a UAV with which multiple tests (weight and visual) were performed. Finally, the comparison of predictions by all the methods is presented including control surface effectiveness with wing-wing interference.作者: BOOST 時間: 2025-3-25 15:35 作者: 違反 時間: 2025-3-25 19:40 作者: faction 時間: 2025-3-25 21:15
7樓作者: LOPE 時間: 2025-3-26 02:20
8樓作者: 朦朧 時間: 2025-3-26 08:18
8樓作者: notification 時間: 2025-3-26 09:32
8樓作者: ATRIA 時間: 2025-3-26 14:09
9樓作者: 貴族 時間: 2025-3-26 19:41
9樓作者: miniature 時間: 2025-3-27 00:12
9樓作者: Condyle 時間: 2025-3-27 03:59
9樓作者: exhibit 時間: 2025-3-27 07:57
10樓作者: 陶醉 時間: 2025-3-27 13:12
10樓作者: Lice692 時間: 2025-3-27 14:21
10樓作者: 增減字母法 時間: 2025-3-27 18:44
10樓
